N913EV

Service difficulty reports · 182

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N913EV' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWIA2026102177791Landing Gear · warning messageGEAR DISAGREE ON TAKEOFF QRH RESOLVED ISSUEC MEL 32-30-1CAT A DUE ONE FLIGHT DAY FROM 102126CAT II DOWNGRADEDRT MLG GEAR INICATED DASHES. FLIGHT 5317. NOTED RT MLG INDICATED DASHES DEFERRED LANDING GEAR RETRACTION SYSTEM IAW MEL 32-30-1 MX ACTION COMPLIED WIOct 21, 2026 · N913EV · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA2026101677758Structure · damagedFOUND TOOLING DAMAGE AT RT BS 672.20, BEHIND APU SHIELD. BLENDED DAMAGE, PERFORMED UT REMAINING THICKNESS MEASUREMENT IAW NDTM PART 4, 51-00-001, & FOUND TO BE ACCEPTABLE IAW REO 601R-53-61-8661, REV-. PERFORMED EDDY CURRENT INSPECTION OF THE BLENDED AREAS IAOct 16, 2026 · N913EV · Cndair CL6002B19 · APU Cowling/ContainmentSDR SWIA2026101677757Skin · corrodedCORROSION ON FUSELAGE SKIN AROUND APU EXHAUST BETWEEN BS 640 - 682, STRINGERS 12R - 14R. BLENDED CORROSION ON FUSELAGE SKIN AROUND APU EXHAUST, PERFORMED UT REMAINING THICKNESS MEASUREMENT IAW NDTM PART 4, 51-00-001 AND FOUND TO BE ACCEPTABLE IAW REO 601R-Oct 16, 2026 · N913EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2026041575692Warning Message · false activationCABIN ALT CAUTION MESSAGE AT 19,000FT. RAN THROUGH CABIN ALT WARNING QRC, FOLLOWED BY CABIN ALT CAUTION QRH. MASKS DEPLOYED. FA REPORTED WISPY WHITE SMOKE IN CABIN MOST PROMINENT IN AFT PORTION ALONG WITH ELECTRICAL BURNING ODOR. PILOTS ALSO SMELLED ELECTRICAApr 15, 2026 · N913EV · Cndair CL6002B19 · Cabin Pressure Control SystemSDR SWIA2026022475505Support Beam · gougedCARGO DOOR TRACK SUPPORT BEAM ASSY HAS GOUGE AT BS 575.70. REPAIRED THE SUPPORT BEAM IAW REO 601R-53-61-8475, SRM 51-42-06, SRM 51-42-20, SRM 51-42-36, SRM 51-24-16, SRM 51-40-11, SRM 51-21-11, SRM 51-25-06, SRM 51-25-16, SRM 51-42-21.Feb 24, 2026 · N913EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2026031175506Skin · dentedAFT FUSELAGE SKIN, BS 700 BTWN STRINGERS 20L-24L DENTED. ACOMPLISHED WHIT REO 601R-53-61-8482, FOR REPAIR ON AFT FUSELAGE SKIN.Feb 21, 2026 · N913EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2026020475508Skin · damagedRIGHT INBD FLAP HAS 5 DISCREPANT NUT PLATE HOLES ON PANEL 684AB. COMPLETED REPAIR OF DISCREPANT HOLES IAW REO 601R-57-52-2542.Feb 4, 2026 · N913EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2026031175507Skin · dentedAFT FUSELAGE BELOW CARGO DOOR CUT OUT, JUST AFT OF BS 605 BELOW WL 73.50 DENTED. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE ALL EVIDENCE USING STANDARD ACFT PRACTICES. COMPLIED WITH REO 601R-53-61-8479.Jan 4, 2026 · N913EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202308070002Unknown · damagedTROUBLESHOOT L WINDSHIELD HEATING DUE TO REPEAT WRITE-UPS FOR L WSHLD HEAT CAUTION WHILE OPERATING AT ALTITUDE.MCI TYPE: TROUBLESHOOTING PRIORITY 1 (FILED CLOSED)REMOVED AND REPLACED LH WINDSHIELD, ALL OPS CHECKS GOOD AT THIS TIME. SEE CP 26975106 FOR REMOVALAug 2, 2023 · N913EV · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA202266789None · crackedBOOST PUMP SATELLITE HOLE LOCATED AT STGR. 6 AT BL 11.15 HAS CRACK INDICATION AT HOLE #10 ON LH WING AFT LOWER SKIN PLANK. (C-CHECK RO 11/8/2022) REPAIRED BOOST PUMP SATELLITE HOLE LOCATED AT STGR. 6 AT BL 11.15 ON LH WING AFT LOWER SKIN PLANK REF REOOct 4, 2022 · N913EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202266788None · crackedBOOST PUMP SATELLITE HOLES LOCATED BETWEEN STGR. 6 AND STGR. 7 AT BL 11.15 HAVE CRACK INDICATIONS IN HOLES #10 AND #11 ON RH WING AFT LOWER SKIN PLANK. (C-CHECK RO 11/8/2022) OPENED UP BOOST PUMP SATELLITE HOLES #10 AND #11 TO 0.266" DIA., LOCATED ATOct 4, 2022 · N913EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202266787Intercostal · corrodedINTERCOSTAL BELOW PAX DOOR AT STR 21L BETWEEN FS 333 TO FS 349 HAS CORROSION (C-CHECK RO 11/8/2022) REMOVED AND REPLACED CORRODED INTERCOSTAL WITH NEW INTERCOSTAL BELOW PAX DOOR AT STR 21L BETWEEN FS 333 TO FS 349 REF CRJ-200 SRM 53-21-17, CRJ-200 SRM 5Sep 27, 2022 · N913EV · Cndair CL6002B19 · Fuselage Main, KeelSDR SWIA202266786None · corrodedINTERCOSTAL BELOW PAX DOOR AT STR 21L BETWEEN FS 319 TO FS 333 HAS CORROSION (C-CHECK RO 11/8/2022) REMOVED AND REPLACED INTERCOSTAL BELOW PAX DOOR STA STGR 21L BETWEEN F.S. 319 AND 333 WITH NEW, REF CRJ 200 SRM 51-42-06 AND DWG 601R31527 REV AM. COMPLISep 27, 2022 · N913EV · Cndair CL6002B19 · DoorsSDR SWIA202266785None · pluggedDURING REMOVAL OF LH SIDE SEAT TRACK BETWEEN F.S. 409.0+16 AND 409.0+32, FOUND REDUNDANT HOLE THROUGH STRUCTURE AND SEAT TRACK PLUGGED WITH A RIVET. (C-CHECK RO 11/8/2022) REPAIRED REDUNDANT HOLE THROUGH SEAT TRACK STRUCTURE PER MHIRJ REO 601R-53-41-308Sep 24, 2022 · N913EV · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202266784None · crackedCENTER WINDSHIELD POST - LOWER LEFT MOUNT BRACKET IS CRACKED. (MARKED) (C-CHECK RO 11/8/2022) REMOVED AND INSTALLED NEW CENTER WINDSHIELD POST LOWER LEFT MOUNT BRACKET REF CRJ200 SRM51-42-21 AND DWG NO. 601R33007 REV -U COMPLIED WITH 51-900-1003-SKYSep 21, 2022 · N913EV · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202266783None · wornPAX DOOR SEAL STRIKER IS WORN. FLAGGED (C-CHECK RO 11/8/2022) REPAIRED PAX DOOR SEAL STRIKER TO BOMBARDIER REO 601R-53-22-033 REV -D DATED 2014-02-17 REPAIR TYPE 1, CUTOUT OF DAMAGE AND INSTALL REPAIR STRAP. PRESSURE LEAK CHECK GOOD. / COMPLIED WITH SKYSep 20, 2022 · N913EV · Cndair CL6002B19 · DoorsSDR SWIA202266782None · corroded*LH WS58.88 BATT RIB FWD LOWER ATTACH CORRODED (MARKED) (C-CHECK RO 11/8/2022) REMOVED AND INSTALLED NEW ANGLE P/N 601R10205-7 REF CRJ200 SRM 51-42-21 & DWG 601R10205 REV F. / COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRUCTURAL MASep 20, 2022 · N913EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202266781None · cracked*LH WS48.30 BATT RIB CAP CRACKED (MARKED) (C-CHECK RO 11/8/2022) REMOVED AND INSTALLED NEW ANGLE REF CRJ200 SRM 51-42-21 AND DWG 601R10204 REV J. COMPLIED WITH 51-900-1003-SKY.Sep 20, 2022 · N913EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202266780None · corrodedCLEAT FOUND TO HAVE CORROSION DURING REMOVAL OF INNER SKIN COMMON TO INTERCOSTAL DD6 AND FORMER 329.76 (C-CHECK RO 11/8/2022) PAX DOOR CLEAT COMMON TO INTERCOSTAL DD6 AND FORMER 329.76 FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW CRJ200 SRM 51-42Sep 20, 2022 · N913EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202266779Nonskid · corrodedCLEAT FOUND TO HAVE CORROSION DURING REMOVAL OF INNER SKIN COMMON TO INTERCOSTAL DD6 AND FRAME 338.963 (C-CHECK RO 11/8/2022) PAX DOOR CLEAT COMMON TO INTERCOSTAL DD6 AND FRAME 338.963 FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW CRJ200 SRM 51-42Sep 20, 2022 · N913EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202266778None · corrodedCLEAT FOUND TO HAVE CORROSION DURING REMOVAL OF INNER SKIN COMMON TO INTERCOSTAL DD4 AND FORMER 311.75 (C-CHECK RO 11/8/2022) PAX DOOR CLEAT COMMON TO INTERCOSTAL DD4 AND FORMER 311.75 FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW CRJ200 SRM 51-42Sep 20, 2022 · N913EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202266777None · corrodedCLEAT FOUND TO HAVE CORROSION DURING REMOVAL OF INNER SKIN COMMON TO INTERCOSTAL DD4 AND FRAME 320.00 (C-CHECK RO 11/8/2022) PAX DOOR CLEAT COMMON TO INTERCOSTAL DD4 AND FRAME 320.00 FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW CRJ200 SRM51-42-06Sep 20, 2022 · N913EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202266776None · corrodedCLEAT FOUND TO HAVE CORROSION DURING REMOVAL OF INNER FORMER FS338.90 COMMON TO INTERCOSTAL DD5 (C-CHECK RO 11/8/2022) PAX DOOR CLEAT COMMON TO FS338.90 AND INTERCOSTAL DD5 FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06, CRJ200 Sep 20, 2022 · N913EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202266775None · corrodedCLEAT FOUND TO HAVE CORROSION DURING REMOVAL OF INNER FORMER FS338.90 COMMON TO INTERCOSTAL DD4 (C-CHECK RO 11/8/2022) PAX DOOR CLEAT COMMON TO FS338.90 AND INTERCOSTAL DD4 FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06, SRM 51-Sep 20, 2022 · N913EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202266774None · corrodedCLEAT FOUND TO HAVE CORROSION DURING REMOVAL OF INNER FORMER FS338.90 COMMON TO INTERCOSTAL DD3 (C-CHECK RO 11/8/2022) PAX DOOR CLEAT COMMON TO FS338.90 AND INTERCOSTAL DD3 FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06, CRJ200 Sep 20, 2022 · N913EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202266773None · corrodedCLEAT FOUND TO HAVE CORROSION DURING REMOVAL OF INNER FORMER FS338.90 COMMON TO INTERCOSTAL DD2 (C-CHECK RO 11/8/2022) PAX DOOR CLEAT COMMON TO FS338.90 AND INTERCOSTAL DD2 WAS FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06, CRSep 20, 2022 · N913EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202266772None · damagedREPAIR TO FS 280.0 BULKHEAD AT LBL 20.75 - RBL 20.75 REQUIRED PER BOMBARDIER REO 601R-53-11-926 REV B DATED 2006/05/10 (C-CHECK RO 11/8/2022) REPAIRED FS 280.0 BULKHEAD AT LBL 20.75 - RBL 20.75 REQUIRED PER BOMBARDIER REO 601R-53-11-926 REV B DATESep 20, 2022 · N913EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202266771None · corrodedPAX DOOR ENTRY BOTH FWD AND AFT CUPS ON FUSELAGE FLOOR SUPPORT HAVE CORROSION. L/H SIDE (C-CHECK RO 11/8/2022) REMOVED AND REPLACED CAPS P/N 601R31527-217 AND CLEATS P/N 601R31527-137. REF CRJ200 SRM 51-42-06 AND DWG 601R31527 REV AM COMPLIED WITH 51-90Sep 20, 2022 · N913EV · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202266770None · corrodedL/H SIDE AT AFT LOWER CORNER OF PAX DOOR ENTRY JUST AFT, AT STRAP AT FS 349.0 THERE IS EXFOLIATION. (C-CHECK RO 11/8/2022) CORROSION ON JOINT BRACKET AT F.S. 349.0 FOUND OUT OF LIMITS OF CRJ 200 SRM, REMOVED AND REPLACED JOINT BRACKET AT FS349.00 P/N: 6Sep 20, 2022 · N913EV · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202266769None · crackedR/H SIDE LWR FWD BOTTOM CORNER OF SERVICE DOOR AT FS 319.70 SUPPORT STRAP HAS A SUSPECT CRACK. (C-CHECK RO 11/8/2022) REMOVED AND REPLACED WITH NEW SUPPORT STRAP AT RH LWR FWD BOTTOM CORNER OF SERVICE DOOR SURROUND REF CRJ200 SRM 51-42-21 AND DWG 601RSep 20, 2022 · N913EV · Cndair CL6002B19 · Galley DoorsSDR SWIA202266768None · corrodedFS 349.0 AT RBL 36 FLOOR SUPPORT HAS CORROSION.(MARKED) (C-CHECK RO 11/8/2022) REPAIRED FS 349.0 AT RBL 36 FLOOR SUPPORT REF REO 601R-53-21-2745, REV --, DATED 2016-11-18. COMPIED WITH 51-900-1003-SKY SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH ALSep 20, 2022 · N913EV · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202266767None · crackedFS 280 AT APPROX RBL 11.0 UNDER FLOOR FWD OF FLOOR SUPPORT STIFFNER HAS SUSPECT CRACK. (C-CHECK RO 11/8/2022) REMOVED AND REPLACED CRACKED FLOOR SUPPORT STIFFENER AT FS 280 APPROX RBL 11.0 UNDER FLOOR FWD SIDE WITH NEW PN 600-34017-724 PO # T-68095 PERSep 20, 2022 · N913EV · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202266766None · crackedFS 280 FWD FLOOR SUPPORT HAS CRACKS AT UPPER RADIUS AT LBL 9.0 AND RBL 9.0 (C-CHECK RO 11/8/2022) REMOVED AND INSTALLED NEW FLOOR SUPPORT ANGLE P/N 600-34017-351 REF CRJ 200 SRM 51-42-06 / BOMBARDIER DWG 600-34017 REV AD. COMPLIED WITH 51-900-1003-SKSep 20, 2022 · N913EV · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202266765None · corrodedCORROSION FOUND ON INNER CLIP AT FS338.90 DURING REMOVAL OF PAX DOOR INNER FORMER AT FS 338.90 (C-CHECK RO 11/8/2022) PAX DOOR CLEAT COMMON TO FRAME 338.90 FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW CRJ200 SRM51-42-06 & CRJ200 SRM 51-42-13, NOSep 19, 2022 · N913EV · Cndair CL6002B19 · DoorsSDR SWIA202266764None · corrodedCORROSION FOUND AT PAX DOOR FORMER FS329.76 DURING SKIN REMOVAL (C-CHECK RO 11/8/2022) PAX DOOR FORMER FS329.76 FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED REF CRJ200 SRM51-42-06, SRM51-42-21 AND DWG NO. 601R31702 REV -N, COMPLIED WITH 51-900-1003-SSep 18, 2022 · N913EV · Cndair CL6002B19 · DoorsSDR SWIA202266763None · wornUPON REMOVAL OF FITTING AND BEARING ON JOB 2773195 OP 92 CAMP 25473174, FOUND R/H ELEVATOR HINGE FITTING ASSY P/N 600-24043-1 TO BE WORN AND PITTED IN BEARING BORE. REPLACE HINGE FITTING ASSY P/N 600-24043-1. (C-CHECK RO 11/8/2022) REPLACED DAMAGED #Sep 17, 2022 · N913EV · Cndair CL6002B19 · Elevator Tab, Attach FittingsSDR SWIA202266762None · corrodedRBL 46 TO RBL27 FLOOR STRAP CORRODED AT FS 559.0 (C-CHECK RO 11/8/2022) REMOVED AND REPLACED CORRODED FLOORSTRAP WITH NEW AT FS 559.0 RBL 46 - RBL 27 REF BOMBARDIER DWG 601R31025 REV N / CRJ 200 SRM 51-42-06, LEAK CHECK GOOD. / COMPLIED WITH SKYWEST TASSep 17, 2022 · N913EV · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202266761None · corrodedFLOOR STRAP CORRODED FROM LBL 46 TO LBL 27 AT FS 559.0 (C-CHECK RO 11/8/2022) REMOVED AND REPLACED CORRODED FLOORSTRAP WITH NEW AT FS 559.0 LBL 46 - LBL 27 REF BOMBARDIER DWG 601R31025 REV N / CRJ 200 SRM 51-42-06, LEAK CHECK GOOD. / COMPLIED WITH SKYWESep 17, 2022 · N913EV · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202266760None · corrodedLH PRESSURE FLOOR SILL CORRODED FROM FS 409+128 TO FS 559.0 (C-CHECK RO 11/8/2022) COMPLIED WITH REO 601R-53-41-666 REV -C DATED 2012-11-06 ON LH PRESSURE FLOOR SILL BETWEEN FS 409+128 AND FS 559.00, COMPLIED WITH 51-900-1003-SKY.SEE CONTINUATION CARD Sep 17, 2022 · N913EV · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202266759None · corrodedUPON REMOVAL OF FITTING AND BEARING ON JOB 2773195 OP 122 CAMP 25501288, FOUND L/H ELEVATOR HINGE FITTING ASSY P/N 600-24043-1 TO HAVE PITTING CORROSION AND EXCESSIVE WEAR IN BEARING BORE. REPLACE HINGE FITTING ASSY. (C-CHECK RO 11/8/2022) REMOVED ASep 17, 2022 · N913EV · Cndair CL6002B19 · Elevator Tab, Attach FittingsSDR SWIA202266758None · damagedDAMAGE HOLES ON PLUG FLAP END ATTACH RH I/B FLAP VANE SKIN AT PANEL 684MB (C-CHECK RO 11/8/2022) REMOVED AND REPLACED RH IB FLAP VANE END PLUG REF CRJ200 SRM 51-42-13 & DWG 601R14302 REV E. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR WORK PSep 15, 2022 · N913EV · Cndair CL6002B19 · Wing, Fuselage Attach FittingsSDR SWIA202266757None · chafedTHE L-H WING INBD FLAP, THE OUTBD LEADING EDGE VANE CAP, HAS CHAFFING (C-CHECK RO 11/8/2022) REMOVED AND REPLACED WITH NEW LEADING EDGE VANE CAP REF CRJ200 SRM 51-42-13 AND DRAWING #601R14302 REV: E / COMPLIED WITH SKYWEST YASK CARD 51-900-1003-SKY (CL6Sep 15, 2022 · N913EV · Cndair CL6002B19 · Wing, Fuselage Attach FittingsSDR SWIA202266756None · chafedTHE L-H WING INBD FLAP, THE MID LEADING EDGE VANE CAP, HAS CHAFFING (C-CHECK RO 11/8/2022) REMOVED AND REPLACED WITH NEW MID LEADING EDGE VANE CAP. P/N 601R14303-51 ON ON L-H WING INBD FLAP PER CRJ200. SRM 51-42-13 REV. 39 DATE MAR 10/21 AND DRAWING. 6Sep 15, 2022 · N913EV · Cndair CL6002B19 · Wing, Fuselage Attach FittingsSDR SWIA202266755None · chafedTHE L-H WING INBD FLAP, THE INBD LEADING EDGE VANE CAP, HAS CHAFFING (C-CHECK RO 11/8/2022) REMOVED AND REPLACED LH IB FLAP, INBD LE VANE CAP WITH NEW, REF CRJ 200 SRM 51-42-13 AND DWG 601R14303 REV J. / COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY Sep 15, 2022 · N913EV · Cndair CL6002B19 · Wing, Fuselage Attach FittingsSDR SWIA202266754None · corrodedCORROSION FOUND AT PAX DOOR INTERCOSTAL 601R318052-1 DURING REMOVAL OF INNER SKIN. (C-CHECK RO 11/8/2022) PAX DOOR INTERCOSTAL 601R318052-1 FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED REF CRJ200 SRM 51-42-06 & DWG &601R31702 REV -N, COMPLIED WITH 51Sep 14, 2022 · N913EV · Cndair CL6002B19 · DoorsSDR SWIA202266753None · corrodedCORROSION FOUND AT PAX DOOR INTERCOSTAL 601R31902-317 DURING REMOVAL OF INNER SKIN (C-CHECK RO 11/8/2022) PAX DOOR INTERCOSTAL 601R31902-317 FOUND TO BE OUT OF LIMITS,REMOVED AND REPLACED WITH NEW IAW CRJ200 SRM 51-42-06 & DWG 601R31702 REV -N, COMPLIEDSep 14, 2022 · N913EV · Cndair CL6002B19 · DoorsSDR SWIA202266752None · corrodedCORROSION FOUND AT PAX DOOR INNER FORMER FS338.90 DURING REMOVAL OF INNER SKIN (C-CHECK RO 11/8/2022) REMOVED AND REPLACED PAX DOOR FORMER AT FS 338.90 WITH NEW, REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 & DWG 601R31702 REV -N. LEAK CHECK GOOD. / COMSep 14, 2022 · N913EV · Cndair CL6002B19 · DoorsSDR SWIA202266751None · crackedAFT CARGO L/H SIDE INNER FUSELAGE AT FS 605.0 ( STR9L FRAME IS CRACKED AT LOWER AND UPPER RIVET LOCATION OF FRAME). (C-CHECK RO 11/8/2022) REPAIRED CRACK TO LH FUSELAGE 605.0 FRAME AT STGR 9L TO BOMBARDIER REO 601R-53-61-5214 REV -A DATED 2016-11-04, FRSep 14, 2022 · N913EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202266750None · gougedSKIN GOUGED / DENTED ON AFT. FUSE., FS589.0+6", RSTR. 25+4.5".REPAIRED SKIN GOUGED / DENT AT FS589.0+6", RSTR. 25+4.5". TO MHIRJ REO 601R-53-61-7900 REV -- DATED 2022-10-17, PATCH REPAIR AT DEFECT AREA, PRESSURE LEAK CHECK GOOD. / COMPLIED WITHY SKYWEST TASK Sep 12, 2022 · N913EV · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202266749None · dented2 OUTWARD DENTS, AFT FUSE. FS654.50+11", LSTR.22+4 (C-CHECK RO 11/8/2022) FUSELAGE SKIN REPAIRED ON FS 654.50+11 AT STRINGER 22LH PER CRJ-200 SRM 53-00-31 PAGES 201-211 REPAIR #3. SEE CONTINUE CARD FOR DETAILS. COMPLID WITH 51-900-1003-SKYSep 12, 2022 · N913EV · Cndair CL6002B19 · Fuselage Structure (General)
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